Nonlinear Thermoelastic Effects on Hypersonic Stability and Control: Part II, Analytical and Experimental Statis Aerothermoelasticity

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Report Number: FDL TDR 64-16 Part 2
Author(s): Batt, James R., Gallagher, Richard H.
Corporate Author(s): Bell Aerosystems Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-10
Pages: 92
Contract: AF 33(657)-7486
DoD Project: 8219
DoD Task: 821901
Identifier: AD0608476

An analytical method was developed for the analysis of static aerothermoelastic behavior in the presence of nonlinear aerodynamic loads and geometrically nonlinear structural behavior. The method was programmed for the IBM 7090 digital computer using FORTRAN coding techniques. A system for the experimental determination of static aerothermoelastic response of nonuniformly heated structures to loadings which are a nonlinear function of wing surface slopes was developed. Results of this experimental program are presented and compared with theoretical predictions.

Provenance: Lockheed Martin Missiles & Fire Control

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